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22篇 您的检索式：作者名="SAYMA A I"

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	题名	作者	年代	出处	被引量
1	Mechanisms and prediction methods for fan blade stall flutter显示文摘	Vahdati M Sayma A I Marshall J G	2001	Journal of Propulsion and Power2001，17，5：	1
2	The effect of stagger variability in gas turbine fan assemblies显示文摘	Wilson M J Imregun M Sayma A I	2007	Journal of Turbomachinery2007，129，2：	1
3	The effect of stagger variability in gas turbine fan assemblies显示文摘	Wilson M J Imregun M Sayma A I	2007	Journal of Turbo Machinery2007，129，2：	1
4	An Integrated Nonlinear Approach for Turbomachinery Forced Response Prediction, Part I: Formulation显示文摘	Sayma A I Vahdati M Imregun M	2000	Journal of Fluids and Structures2000，14，1：	1
5	An Integrated Nonlinear Approach for Turbomachinery Forced Response Prediction, Part II: Case Studies显示文摘	Vahdati M Sayma A I Imregun M	2000	Journal of Fluids and Structures2000，14，1：	1
6	An Integrated Nonlinear Approach for Turbomachinery Forced Response Prediction,Part I: Formulation显示文摘	Vahdati M Imregun M	2000	Journal of Fluids and Structures2000，14，：	1
7	An integrated nonlinear approach for turbomachinery forced response prediction, part I: formulation 显示文摘	SAYMA A I VAHDATI M IMREGUN M	2000	Journal of Fluids and Structures2000，14，：	1
8	An integrated nonlinear approach for turbo machinery forced response prediction, part I: formulation显示文摘	Sayma A I Vahdati M Imregun M	2000	Journal of Fluids and Structures2000，14，1：	1
9	Multibladerow forced response modeling in axial-flow core compressors显示文摘	Vahdati M Sayma A I Imregun M	2007	Journal of Turbomachinery2007，129，2：	1
10	Aeroelasticity analysis of air - riding seals for aero - engine applications 显示文摘	Sayma A I Breard C Vahdati M and Imregun M	2002	Journal of Tribology2002，124，：	1
11	On the use of at mospheric boundary conditions for axial-flow compressor stall simulations显示文摘	Vahdati M Sayma A I Freeman C	2005	Journal of Turbomaehinery2005，127，2：	1
12	The effect of stagger variability in gas turbine fan assemblies显示文摘	WILSON M J IMREGUN M SAYMA A I	2007	Journal of Turbomachinery2007，129，2：	1
13	The effect of stagger variability in gas turbine fan assemblies 显示文摘	Wilson M J Imregun M Sayma A I	2007	Journal of Turbomachinery2007，129，2：	1
14	On the Use of Atmospheric Boundary Conditions for Axial-Flow Compressor Stall Simulations显示文摘	Vahdati M Sayma A I Freeman C	2005	ASME J Turbomachinery2005，127，2：	1
15	The Effect of Stagger Variability in Gas Turbine Fan Assemblies显示文摘	Wilson M J Imregun M Sayma A I	2007	Journal ofTurbomachinery2007，129，2：	1
16	Mechanismsand prediction methods for fan blade stall flutter显示文摘	Vahdati M Sayma A I Marshall J G	2001	Jour-nal of Propulsion and Power2001，17，5：	1
17	Mechanisms and prediction methods for fan blade stall flutter显示文摘	Vahdati M Sayma A I Marshall J G	2001	Jour- nal of Propulsion and Power2001，17，5：	1
18	Multi-bladerow fan forced response predictions using an integrated three-di- mensional time-domain aeroelasticity model显示文摘	Sayma A I Vahdati M Imregun M	2000	Journal of Mechanical Engineering Science2000，214，12：	1
19	On the use of atmospheric boundary conditions for axialflow compressor stall simulations显示文摘	Vahdati M Sayma A I Freeman C	2005	ASME Journal of Turbomachinery2005，127，：	1
20	Semi - unstructured mesh generator for flow calculations in axial turbomachinery blading 显示文摘	Sbardella L Sayma A I Imergun M	2000	Journal for Numerical Method in Fluids2000，32，5：	1

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